Abstract
We performed a numerical study of the boundary layer on a wall in a supersonic gas flow using a differential turbulence model. The dependences of the recovery factor and the Reynolds analogy factor on the main flow parameters, such as the Reynolds, Mach, and Prandtl numbers, are obtained for a series of the temperature factor values. The results of calculations are approximated by the dependences of the recovery factor and the Reynolds analogy factor on the Prandtl number.
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Original Russian Text © V.G. Lushchik, M.S. Makarova, 2016, published in Teplofizika Vysokikh Temperatur, 2016, Vol. 54, No. 3, pp. 401–407.
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Lushchik, V.G., Makarova, M.S. Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate. High Temp 54, 377–382 (2016). https://doi.org/10.1134/S0018151X16030111
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DOI: https://doi.org/10.1134/S0018151X16030111